| KEYWORD |
11 - LAQ AerMec per componenti di turbine e compressori
Innovative layout for a bladed-disk to be used in a Low Pressure turbine for aeronautical application, trade-off study and feasibility assessment
Thesis in external company
keywords BLADED DISK DYNAMICS, TURBINE
Reference persons DANIELE BOTTO
Research Groups 11 - LAQ AerMec per componenti di turbine e compressori
Thesis type MASTER THESIS
Description This activity will analyze different Air Flow layout which will possibly increase the design space on a LPT row on an Engine. This A/F will be evaluated from both a mechanics and aeromechanics point of view in order to perform a complete trade-off for the different design alternatives available.
Required skills MS engineering students (energy, aerospace, mechanical or equivalent).
Bonus: Finite Element Analysis and vibration mechanics.
Notes Duration: 8 months
Location of the internship: GE-AVIO
Deadline 09/03/2020
PROPONI LA TUA CANDIDATURA